CONCERNING THE PROBLEM OF THE FLOW OF A HYPERSONIC STREAM OF GAS AROUND A THIN BODY,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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The hypersonic flow of an ideal gas over slender bodies is discussed. The flow Mach number is assumed to be infinite and is directed along the x-axis. Nondimensional coordinates are introduced, and a boundary value problem is obtained in nondimensional form.
- Fluid Mechanics